Revision: 6

Date: 11/30/2006

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

LR-24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 35, 35A,                           36, 36A, 55, 55B, 55C

Roman A. Buettner

Chairman, Flight Operations Evaluation Board

(FOEB)

Federal Aviation Administration Aircraft Evaluation Group DOT Building, Room 332 901 Locust       Street Kansas City, MO                    64106-2641

Telephone:   (816)-329-3233

FAX:   (816)-329-3241

  --

--

--

--

--

--

--

--

--

--

--

21

22

24-1

26

27

29-1

30

31

32-1

33

35-1

52-1

73-1

77-1

78-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

I

TABLE OF CONTENTS

SYSTEM

SYSTEM NO.

PAGE NO.

Table of Contents

Log of Revisions

I

II, III, IV

Control Page

Highlights of Change

V, VI, VII

VIII, IX, X

Highlights of Change

Definitions

XI, XII

XIII, XIV, XV,

Definitions

Definitions

XVI, XVII, XVIII,

XIX, XX, XXI

-- Preamble

XXII, XXIII

XXIV, XXV, XXVI,

Guidelines for (O) & (M) Procedures Guidelines for (O) & (M) Procedures

XXVII, XXVIII,

XIX, XXX

Guidelines for (O) & (M) Procedures Air Conditioning

21-1 THRU 7

22-1, 2, 3

Auto Flight

23 Communications

23-1 THRU 6

24 Electrical Power

25 Equipment/Furnishings

25-1 THRU 7

26-1, 2

Fire Protection

Flight Controls

27-1, 2

28-1 THRU 7

28 Fuel

29 Hydraulic Power

Ice and Rain Protection

Indicating/Recording Systems

30-1, 2, 3

31-1, 2

32 Landing Gear

Lights

33-1, 2, 3, 4

34-1 THRU 16

34 Navigation

35 Oxygen

38 Water/Waste

52 Doors

38-1, 2

73 Engine/Fuel Controls

77 Engine Indicating

78 Engine Exhaust

DEPARTMENT OF TRANSPORTATION

  2

2

2

2

2

2

2

2

2

2

2

2

3

3

3

3

3

3

3

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

Original 04/26/1988 Original Issue

Oa

07/15/1991

HIGHLIGHTS OF REV.

1 04/22/1992 ALL PAGES

1a

04/14/1993

HIGHLIGHTS OF REV.

25-1, 25-2, 25-3

1a

04/14/1993

07/14/1993

HIGHLIGHTS OF REV., DEFINITIONS

2 07/14/1993 GUIDELINES

07/14/1993

21-1, 21-2, 21-3, 21-4, 21-5

21-6, 21-7, 21-8, 22-1, 22-2

07/14/1993

07/14/1993

23-1, 23-2, 23-3, 24-1, 24-2

24-3, 25-1, 25-2, 25-3, 26-1

07/14/1993

07/14/1993

26-2, 27-1, 27-2, 28-1, 28-2

28-3, 28-4, 28-5, 28-6, 28-7

07/14/1993

07/14/1993

28-8, 29-1, 30-1, 30-2, 30-3

30-4, 31-1, 32-1, 33-1, 33-2

07/14/1993

07/14/1993

33-3, 33-4, 33-5, 34-1, 34-2

34-3, 34-4, 34-5, 34-6, 34-7

07/14/1993

07/14/1993

35-1, 52-1, 73-1, 77-1, 78-1

HIGHLIGHTS OF REV.

2a

2a 08/19/1994 34-7

08/19/1994

02/07/1995

3 02/07/1995 GUIDELINES

HIGHLIGHTS OF REV., DEFINITIONS

02/07/1995

02/07/1995

21-1, 21-2, 21-4, 21-5, 21-6

21-7, 21-8, 23-2, 23-3, 24-1

02/07/1995

02/07/1995

25-1, 25-3, 26-1, 26-2, 27-1

27-2, 28-3, 28-6, 31-1, 33-1

02/07/1995

02/07/1995

33-2, 33-3, 34-2, 34-3, 34-4

34-5, 34-6, 34-7, 34-8

3a

3a 06/12/1996 GUIDELINES

06/12/1996

HIGHLIGHTS OF REV., DEFINITIONS

3a

3a

06/12/1996

06/12/1996

21-1, 21-2, 21-4, 21-5, 21-6

21-7, 21-8, 23-2, 23-3, 23-4

3a

3a

06/12/1996

06/12/1996

25-1, 25-3, 26-2, 27-1, 27-2

28-4, 33-2, 33-3, 34-2, 34-3

3a

3b

06/12/1996

12/23/1997

34-4, 34-5, 34-6, 34-7, 34-8

HIGHLIGHTS OF REV., DEFINITIONS

3b 12/23/1997 GUIDELINES

3b

12/23/1997

22-2, 23-4, 77-1

3c

3c 02/25/2000 PREAMBLE, GUIDELINES

02/25/2000

HIGHLIGHTS OF REV., DEFINITIONS

3c

3c

02/25/2000

02/25/2000

21-1, 21-2, 21-3, 21-4, 22-2

23-4, 24-1, 28-8, 31-1, 33-4

3c

02/25/2000

33-5, 34-5, 34-8, 34-9, 77-1

DEPARTMENT OF TRANSPORTATION

  4

4

4

4

4

4

4

4

4

4

4

4

4

4

5

5

5

5

5

5

5

5

5

5

6

6

6

6

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

III

Log of Revisions

Rev No.

Date

Page Numbers

Initials

3c 02/25/2000 78-1

04/04/2002

HIGHLIGHTS OF REV., DEFINITIONS

4 04/04/2002 GUIDELINES

04/04/2002

21-1, 21-2, 21-3, 21-4, 21-5

21-6, 21-7, 21-8, 22-1, 22-2

04/04/2002

04/04/2002

23-1, 23-2, 23-3, 23-4, 23-5

23-6, 24-1, 24-2, 25-1, 25-2

04/04/2002

04/04/2002

25-3, 26-1, 26-2, 27-1, 27-2

28-1, 28-2, 28-3, 28-4, 28-5

04/04/2002

04/04/2002

28-6, 28-7, 28-8, 29-1, 30-1

30-2, 30-3, 30-4, 31-1, 31-2

04/04/2002

04/04/2002

32-1, 33-1, 33-2, 33-3, 33-4

33-5, 34-1, 34-2, 34-3, 34-4

04/04/2002

04/04/2002

34-5, 34-6, 34-7, 34-8, 34-9

34-10, 34-11, 34-12, 34-13

04/04/2002

04/04/2002

35-1, 38-1, 52-1, 73-1, 77-1, 78-1

HIGHLIGHTS OF REV., DEFINITIONS

4a

4a

GUIDELINES

21-2, 21-3, 21-6, 21-7, 21-8

4a

4a

22-1, 22-2, 23-1, 23-2, 23-3

23-4, 23-5, 23-6, 25-1, 25-2

4a

4a

25-3, 27-1, 27-2, 28-2, 28-3

28-5, 28-6, 28-8, 30-3, 30-4

4a

4a

33-1, 33-2, 33-3, 33-4, 33-5

34-1, 34-3, 34-4, 34-5, 34-6

4a

4a

34-7, 34-8, 34-9, 34-10, 34-11

34-12, 34-13, 38-1

4a

11/22/2002

5 11/22/2002 GUIDELINES

HIGHLIGHTS OF REV., DEFINITIONS

11/22/2002

11/22/2002

21-2, 21-3, 21-6, 21-7, 21-8

22-1, 22-2, 23-1, 23-2, 23-3

11/22/2002

11/22/2002

23-4, 23-5, 23-6, 25-1, 25-2

25-3, 27-1, 27-2, 28-2, 28-3

11/22/2002

11/22/2002

28-5, 28-6, 28-8, 30-1, 30-3

30-4, 33-1, 33-2, 33-3, 33-4

11/22/2002

11/22/2002

33-5, 34-1, 34-3, 34-4, 34-5,

34-6, 34-7, 34-8, 34-9, 34-10

11/22/2002

11/30/2006

34-11, 34-12, 34-13, 38-1

HIGHLIGHTS OR REV., DEFINITIONS

6 11/30/2006 GUIDELINES, PREAMBLE

11/30/2006

21-1, 21-2, 21-5, 22-1, 22-2

11/30/2006

11/30/2006

22-3, 23-1, 23-2, 23-3, 23-5

23-6, 25-1, 25-2, 25-3, 25-4

DEPARTMENT OF TRANSPORTATION

  6

6

6

6

6

6

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

IV

Log of Revisions

Rev No.

Date

Page Numbers

Initials

11/30/2006

11/30/2006

25-5, 25-6, 25-7, 26-1, 26-2

27-1, 28-5, 30-1, 30-2, 31-2

11/30/2006

11/30/2006

32-1, 33-2, 34-1, 34-2, 34-5

34-6, 34-7, 34-8, 34-9, 34-10

11/30/2006

11/30/2006

34-11, 34-12, 34-13, 34-14

34-15, 34-16, 35-1, 38-2

DEPARTMENT OF TRANSPORTATION

  -

6

6

6

6

6

6

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

V

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

Table of Contents

11/30/2006

11/30/2006

I

II

Log of Revisions

11/30/2006

III 6 11/30/2006

IV 6 11/30/2006

V

11/30/2006

Control Page

VI 6 11/30/2006

VII 6 11/30/2006

Highlights of Change

VIII

IX

11/30/2006

6 11/30/2006 6 11/30/2006 X

XI 6 11/30/2006 XII 6 11/30/2006 Definitions XIII 10 05/12/2006 XIV 10 05/12/2006 XV 10 05/12/2006 XVI 10 05/12/2006 XVII 10 05/12/2006 XVIII 10 05/12/2006 XIX

                          10 05/12/2006 XX 10 05/12/2006 XXI 10 05/12/2006 Preamble XXII 2 06/14/1989 XXIII 2 06/14/1989

Guidelines for (O) & (M) Procedures

XXIV

XXV 6 11/30/2006

11/30/2006

XXVI 6 11/30/2006

XXVII 6 11/30/2006

XXVIII 6 11/30/2006

XXIX 6 11/30/2006

XXX 6 11/30/2006

21 21-1 6 11/30/2006

21-2 6 11/30/2006

21-3 5 11/22/2002

21-4 4 04/04/2002

21-5 6 11/30/2006

21-6 5 11/22/2002

21-7 5 11/22/2002

22 22-1 6 11/30/2006

22-2 6 11/30/2006

22-3 6 11/30/2006

23 23-1 6 11/30/2006

23-2 6 11/30/2006

23-3 6 11/30/2006

DEPARTMENT OF TRANSPORTATION

  23-4

5

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

VI

Control Page

System

Page No.

Rev. No.

Current Date

Control Page (continued)

23 (continued)

11/22/2002

23-5 6 11/30/2006

23-6 6 11/30/2006

24 24-1 4 04/04/2002

25 25-1 6 11/30/2006

25-2 6 11/30/2006

25-3 6 11/30/2006

25-4 6 11/30/2006

25-5 6 11/30/2006

25-6 6 11/30/2006

25-7 6 11/30/2006

26 26-1 6 11/30/2006

26-2 6 11/30/2006

27 27-1 6 11/30/2006

27-2 5 11/22/2002

28 28-1 4 04/04/2002

28-2 5 11/22/2002

28-3 5 11/22/2002

28-4 5 11/22/2002

28-5 6 11/30/2006

28-6 4 04/04/2002

28-7 5 11/22/2002

29 29-1 4 04/04/2002

30 30-1 6 11/30/2006

30-2 6 11/30/2006

30-3 5 11/22/2002

31 31-1 4 04/04/2002

31-2 6 11/30/2006

32 32-1 6 11/30/2006

33 33-1 5 11/22/2002

33-2 6 11/30/2006

33-3 5 11/22/2002

33-4 5 11/22/2002

34 34-1 6 11/30/2006

34-2 6 11/30/2006

34-3 5 11/22/2002

33-4 5 11/22/2002

34-5 6 11/30/2006

34-6 6 11/30/2006

34-7 6 11/30/2006

34-8 6 11/30/2006

34-9 6 11/30/2006

DEPARTMENT OF TRANSPORTATION

  34-10

6

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

VII

Control Page

System

Page No.

Rev. No.

Current Date

Control Page (Continued)

34 (continued)

11/30/2006

34-11 6 11/30/2006

34-12 6 11/30/2006

34-13 6 11/30/2006

34-14 6 11/30/2006

34-15 6 11/30/2006

34-16 6 11/30/2006

35 35-1 6 11/30/2006

38 38-1 5 11/22/2002

38-2 6 11/30/2006

52 52-1 4 04/04/2002

73 73-1 4 04/04/2002

77 77-1 4 04/04/2002

78 78-1 4 04/04/2002

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

VIII

HIGHLIGHTS OF CHANGE

Definitions

Updated in accordance with Policy Letter 25, Global Change 142.

Guidelines

[(O) &(M)]

Updated IAW applicable Policy Letter Provisos and/or Industry requests.

ATA 21-1-1

“And” changed to “or” between items “a” & “b” in the second part of the proviso.

ATA 21-1-2

“And” changed to “or” between items “a” & “b” in the second part of the proviso.

ATA 21-1-3

Provisos updated at manufacturer’s request and abbreviation for “passenger” (PASS) in NOTE corrected.

ATA 21-12

“Indicating” changed to “Indicator” in System Item Description.

ATA 22-1-1

Revised Autopilot System relief in accordance with PL-101 (GC-103) and added NOTE 2 for RVSM operations restriction.

ATA 22-1-2

Added relief for aircraft with two or more Autopilots installed IAW PL-101 (GC-103) and added NOTE 2 for RVSM operations restriction.

ATA 22-3

Relief added for Autopilot Disconnect IAW PL-93.

ATA 23-5

System Item Description changed to comply with PL-9 (GC-119).

ATA 23-5-2

Proviso changed to comply with PL-9 (GC-119).

ATA 23-9

Updated to comply with PL-117 (GC-137).

ATA 23-9-1

Updated to comply with PL -117 (GC-137).

ATA 23-11-1

Updated to comply with PL-29 (GC-128).

ATA 23-11-2

Updated to comply with PL-29 (GC-128).

ATA 23-11-3

Updated to comply with PL-29 (GC-128).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

IX

HIGHLIGHTS OF CHANGE

ATA 23-15

Updated to comply with PL-106 (GC-135).

ATA 23-16

Boom Microphone relief revised IAW PL-58 (GC-100).

ATA 23-17

Relief added for Crew Intercoms per Industry request.

ATA 25-1

Revised to comply with PL-79 (GC-134).

ATA 25-1-1

Revised to comply with PL-79 (GC-134).

ATA 25-1-2

Revised to comply with PL-79 (GC-134).

ATA 25-1-3

Revised to comply with PL-79 (GC-134).

ATA 25-1-4

Item moved from 25-1-3 to 25-1-4.

ATA 25-4

Proviso wording updated to comply with PL-89.

ATA 25-5

Updated to comply with PL-116 (GC-138).

ATA 25-6

Revised to comply with PL-100 (GC-114).

ATA 25-7

“EMS” abbreviation in System Item Description spelled out.

ATA 25-8

Updated to comply with PL-56 (GC-127).

ATA 25-8-1

Updated to comply with PL-56 (GC-127).

ATA 25-9

Updated to comply with PL-73 (GC-144).

ATA 25-9-1

Updated to comply with PL-73 (GC-144).

ATA 25-9-2

Updated to comply with PL-73 (GC-144).

ATA 25-9-3

Updated to comply with PL-73 (GC-144).

ATA 25-10

Number required for Dispatch and Remarks or Exceptions revised for ELT.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

X

HIGHLIGHTS OF CHANGE

ATA 25-11

Relief added for Exterior Lavatory Door Ashtrays IAW PL-85 (GC-80).

ATA 25-11-1

Relief added for Exterior Lavatory Door Ashtrays IAW PL-85 (GC-80).

ATA 25-11-2

Relief added for Exterior Lavatory Door Ashtrays IAW PL-85 (GC-80).

ATA 25-12

Relief added for Galley Waste Receptacle Access Doors/Covers IAW PL-96 (GC-98).

ATA 25-13

Relief added for Cabin and Galley Storage Compartments and Closets IAW PL-104 (GC-129).

ATA 26-3

Paragraph “b)” deleted in proviso per manufacturer’s request and revised IAW PL-24 (GC-106).

ATA 26-4

Paragraph “b)” deleted at manufacturer’s request and revised to comply with PL-24 (GC-106).

ATA 26-5

Updated to comply with PL-75 (GC-53).

ATA 26-6

Added to comply with Pl-102 (GC-77).

ATA 27-6

Revised relief for Flap Preselect System to include operations of Lear 35/36 Models with Flap Control Bypass System IAW SB35/36-27-31 per manufacture’s proposal.

ATA 28-4-1

Updated per manufacture’s proposal.

ATA 28-4-2

Updated per manufacturer’s proposal.

ATA 28-5

System Item Description revised for Single Point Pressure Refueling (SPPR) System.

ATA 30-3

Temperature reference in proviso changed from +4 C to +10 C.

ATA 30-4

Temperature reference in proviso changed from + 4 C to +10 C.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XI

HIGHLIGHTS OF CHANGE

ATA 30-5

Temperature reference in proviso changed from +4 C to +10 C.

ATA 30-6

Temperature reference in proviso changed from +4 C to +10 C.

ATA 31-3-3

Flight Data Recorder relief added for operators other than the holder of an Air Carrier or Commercial Operator Certificate IAW PL-87 (GC-136).

ATA 32-1

Item “c)” in Anti-Skid System proviso reworded.  No change in relief.

ATA 33-9

System Item Description revised to comply with PL-77 (GC-63).

ATA 34-1

Standby Attitude Indicator relief revised IAW PL-111.

ATA 34-8

Transponder/Altitude Reporting Systems relief revised IAW PL-76 (GC-133).

ATA 34-22

TCAS I relief updated IAW PL-32 (GC-145).

ATA 34-23

TCAS II relief updated IAW PL-32 (GC-145).

ATA 34-23-1

TCAS II Sub-System updated IAW PL-32 (GC-145).

ATA 34-23-4

TCAS II Sub-System added IAW PL-32 (GC-145).

ATA 34-23-5

TCAS II Sub-System added IAW PL-32 (GC-145).

ATA 34-27

System Item Description abbreviation spelled out.

ATA 34-28

System Item Description abbreviation spelled out.

ATA 34-29

System Item Description abbreviation spelled out.

ATA 34-30

System Item Description abbreviation spelled out.

ATA 34-31

Deleted, Revision 6.

ATA 34-38

Entire TAWS relief revised IAW PL-54 (GC-139).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, 28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XII

HIGHLIGHTS OF CHANGE

ATA 34-39

Entire Wind Shear Detection, Guidance and Avoidance System(s) relief revised IAW PL-67 (GC-140).

ATA 34-40-1

Typo removed.

ATA 34-42

“***” removed from System Item Description to comply with PL- 105 (GC-86).

ATA 34-44

Traffic Advisory System (TAS) relief added per manufacturer’s request.

ATA 35-3

Protective Breathing Equipment relief added to comply with PL-43.

ATA 38-2

Lavatory Waste Systems relief updated to comply with PL-83 (GC-108).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XIII

DEFINITIONS

1. System Definitions.

System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially.

a. "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column.

b. "Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required.

c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

d. "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page.

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet.

3. "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules. The number of items required by the FAR must be operative. When the listed item is not required by FAR it may be inoperative for the time specified by repair category.  The term “14 CFR” may be substituted for “FAR” in MMELs or operator MELs.

4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition.

NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XIV

DEFINITIONS

5."-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.

6. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

7."ER" refers to extended range operations of a two-engine airplane (ETOPS) which has a type design approval for ER operations (ETOPS) and complies with the provisions of Advisory Circular 120-42A.

8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations.

9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction).

11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

12. ”Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s).

13. ”Notes:" in Column 4 provides additional information for crewmember or maintenance consideration. Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements. Notes are not a part of the provisos.

14. Inoperative components of an inoperative system: Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system. (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XV

DEFINITIONS

15. "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL.

16. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as a part of the operator's manual or MEL.

NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the Administrator.

17. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator.

18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules.

20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

21. "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc.

DEPARTMENT OF TRANSPORTATION

  a.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XVI

DEFINITIONS

22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

Category A. Items in this category shall be repaired within the time interval specified in the remarks column of the operator's approved MEL.

Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record.

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system – General

New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be represented. The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status.  When preparing the MEL document, operators are to select the proper Definition No. 23 for their aircraft, if appropriate.

BOEING (B-757/767, B-747-400, B-777)

Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS) provide different priority levels of system messages (WARNING, CAUTION, ADVISORY, STATUS and MAINTENANCE).  Any messages that affects airplane dispatch status will be displayed at a STATUS message level or higher. The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is operating within its approved operating limits or tolerances.

DEPARTMENT OF TRANSPORTATION

  18

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XVII

DEFINITIONS

System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

b. Boeing (B-717, MD-10, MD-11)

These aircraft are equipped with an alerting function which is a subsystem within the Electronic Instrument System (EIS). The alerting function provides various levels of system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS)

Alerts that affect aircraft dispatch will include WARNING, CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are displayed on the status page of the EIS display panel under the maintenance heading.

A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be identified by the Central Fault Display System (CFDS) interrogation. The systems are designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.

c. AIRBUS (A-300-600, A-310, A-318/320/319/321, A-330, A-340)

Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages (WARNING, CAUTION, STATUS, and ADVISORY). A-318/320/319/ 321, A-330, and A-340 also provide MAINTENANCE status messages.

Any message that affects airplane dispatchability will normally be at the WARNING, CAUTION or STATUS level. MAINTENANCE messages (A-318/319/320/321, A-330, and A-340 only) are also indicated on ECAM Status Page below the white Maintenance label.

A MAINTENANCE status (Class II) message on ECAM indicates the presence of a system fault which can be identified by CFDS (A-318/319/320/321) or CMS (A-330/A- 340) interrogation. The systems are designed to be fault tolerant. For A- 318/319/320/321, MAINTENANCE STATUS (Class II) do not affect dispatch but are listed in the MMEL.  Dispatch is allowed without specific conditions except for:

-  BLUE RSVR MAINTENANCE status:  If applicable, and

-  AIR BLEED MAINTENANCE status: As applicable.

For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XVIII

DEFINITIONS

d.  FOKKER (FK-100)

Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides electronic message referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any messages that affects aircraft dispatch will be at the WARNING, CAUTION or AWARENESS level.  In these cases the MEL must be verified for dispatch capability and maintenance may be required.

System conditions that only require maintenance are not ¦presented on the flight deck. These maintenance indications/messages may be presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by dedicated Built in Test Evaluation (BITE) of systems.

e.  CANADAIR  (CL-65, CL-604)

Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAAS) provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.

System conditions that only require maintenance are not visible to the flight crew.  These maintenance indications/messages are only activated by maintenance personnel using the Maintenance Diagnostics Computer.

f.  EMBRAER (EMB-135/145, ERJ-170/190 Series)

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS) that provides three different message levels:  WARNING, CAUTION, and ADVISORY.  The ERJ-170/190 Series add STATUS messages.

Failures that effect dispatchability are presented to the flight crew at one of these levels. Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC).  System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XIX

DEFINITIONS

g.  GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X)

Gulfstream airplanes equipped with EICAS provide different priority levels of system messages:  WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue).  Any WARNING or CAUTION message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  STATUS messages which indicate a system failure (e.g., FMS-1 fail) require that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  Maintenance messages do not affect airplane dispatch status.  They indicate the presence of a system fault which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual.

h.  De- HAVILLAND (DASH 8 SERIES 400)

Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings.  Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in the cockpit.

“Class 1 failures” are failures that prevent continued operation of a specific Line Replacement Unit or channel and are annunciated via advisory messages:  caution, warning or advisory lights in the flight compartment.  Dispatch with such posted failures are to be in accordance with the MMEL.

“Class 2 failures” are failures which do not prevent continued system function.  These faults will not be annunciated to the flight crew and the absence of the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances.  Such faults would be evident during maintenance interrogation performed during maintenance activities.  Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM).  Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

24. "Administrative control item" means an item listed by the operator in the MEL for tracking and informational purposes. It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item.

DEPARTMENT OF TRANSPORTATION

  D."

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XX

DEFINITIONS

25."***" symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft. The symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft.

26. "Excess Items" means those items that have been installed that are redundant to the requirements of the FARs.

27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and

28. “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative.  The item shall not be used or operated until the original deferred item is repaired.  Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

29. “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used.”  In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations.  It is not necessary for the operators to accomplish the (M) procedures associated with the item.  However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not to be used under normal operations.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 10

DATE: 5/12/2006

PAGE NO:

XXI

DEFINITIONS

30. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original certification, supplemental type certificate, or engineering order that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules.  They are those items that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.  These nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories, and galley areas.  NEF items are not items already identified in the MEL or CDL of the applicable aircraft.  They do not include items that are functionally required to meet the certification rule or for compliance with any operational rule.  Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil consumption, etc.  Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 2

DATE: 06/14/1989

PAGE NO:

XXII

PREAMBLE

(06/14/1989)

The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

Equipment not required by the operation being conducted and equipment in excess of FAR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 2

DATE: 06/14/1989

PAGE NO:

XXIII

PREAMBLE

(06/14/1989)

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to operation with any item of equipment inoperative.

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED

DEPARTMENT OF TRANSPORTATION

  21-1-1

(O)

21-1-2

(O)

21-1-3

(O)

21-8

(M)

21-10

(O)

21-11

(O)

22-1-1

(M)

(O)

22-1-2

(M)

(O)

23-4

(O)

23-5

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXIV

Guidelines for (O) & (M) Procedures

The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures:

Operations procedure to operate the aircraft in an unpressurized configuration and ensure Bleed Air is operative and ON.  (Applies to both provisos).

Operations procedure to operate the aircraft in an unpressurized configuration and ensure Bleed Air is operative and ON.  (Applies to both provisos).

Operations procedure to operate the aircraft in an unpressurized configuration and ensure that Override Switches are in OVERRIDE.

Maintenance procedure to verify both Emergency Pressurization Systems are operative.

Operations procedure to evaluate unpressurized operations when flight planning below 9000 feet MSL.

Operations procedure to evaluate unpressurized operations when flight planning below 9000 feet MSL.

Maintenance procedure to determine that Servos do not interfere with the flight controls.

Operations procedure to ensure aircraft is operated in accordance with the AFM and use of Autopilot is not required.

Maintenance procedure to ensure Autopilot is deactivated or secured in a manner to prevent interference with flight controls.

Operations procedure to ensure aircraft is operated in accordance with the AFM Limitations and procedures do not require use of Autopilot.

Operations procedure to ensure Cockpit Speakers are not required.

Operations procedure to ensure alternate, normal and emergency operations are used for passengers.

DEPARTMENT OF TRANSPORTATION

  23-6

(M)

(O)

23-9

(O)

23-9-1

(O)

23-10

(O)

23-15

(O)

23-17

(O)

24-1-1

(M)

(O)

24-2

(O)

25-1-2

(O)

25-3

(M)

25-6

(M)

25-7

(M)

25-9-1

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXV

Guidelines for (O) & (M) Procedures

Maintenance procedure to secure or deactivate affected equipment.

Operations procedure established for use of alternate air/ground communications.

Operations procedure to ensure crew monitors appropriate frequency if required.

Operations procedure to ensure crew monitors appropriate frequency if required.

Operations procedure to ensure alternate passenger briefing procedures are used.

Operations procedure to ensure Long Range Communications Systems (LRCS) as required are available.

Operations procedure to establish other means of communications for normal and emergency flight operations.

Maintenance procedure to deactivate affected Inverter.

Operations procedure to ensure the third Inverter is not required.

Operations procedure to ensure AC Voltmeters are not required.

Operations procedure to ensure baggage is not stowed under any Seat with an inoperative Restraining Bar, Seat is placarded and procedures are established to alert cabin crew of any

inoperative Restraining Bars.

Maintenance procedure to secure or deactivate Drag Chute System.

Maintenance procedure to ensure loading and securing cargo in compliance with an approved source is conducted.

Maintenance procedure to ensure System is deactivated and secured.

Operational procedure to ensure Defibrillator and/or Associated Equipment is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit  and repairs or replacements are made within three flight cycles.

DEPARTMENT OF TRANSPORTATION

  25-9-2

(O)

25-9-3

(O)

25-12

(M)

(O)

25-13

(M)

26-1

(M)

26-3

(M)

(O)

26-4

(M)

(O)

28-1-1

(O)

28-1-2

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXVI

Guidelines for (O) & (M) Procedures

Operational procedure to ensure Emergency Medical Kit and/or Associated Equipment is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit and repairs or replacements are made within three flight cycles.

Operational procedure to ensure First Aid Kit and/or Associated Equipment is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit and repairs or replacements are made within three flight cycles.

Maintenance procedure to ensure Galley Waste Receptacle Container is empty and the Access Door is secured.

Operations procedure to ensure sufficient Galley Waste Receptacles are available to accommodate all waste that may be generated on a flight.

Maintenance procedures to secure affected compartments CLOSED.

Maintenance procedure to ensure associated Bottle charge is adequate.

Maintenance procedure to ensure Lavatory Fire Extinguisher System operates properly and Lavatory Door is placarded.

Operations procedure to ensure Lavatory is used only by the flight crew.

Maintenance procedure to ensure Lavatory Smoke Detection System operates normally and Lavatory Door is placarded.

Operations procedure to ensure Lavatory is used only by the flight crew.

Operations procedure to ensure both Standby Electric Boost Pumps are operative and ON and opposite side Jet Boost Pump System is operative and OFF.

Operations procedure to ensure both Standby Electric Boost Pumps are operative and ON and takeoffs and intentional go-arounds are not conducted with less than 600 pounds of fuel in Wing Tank with inoperative Jet Boost Pump System.

DEPARTMENT OF TRANSPORTATION

  28-6

(O)

28-7

(O)

28-9

(O)

28-10-1

(O)

28-10-2

(O)

28-11

(O)

29-1

(M)

31-2

(O)

(O)

32-1

(M)

(O)

33-7

(O)

33-11-1

(O)

33-14

(M)

34-7

(O)

34-12

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXVII

Guidelines for (O) & (M) Procedures

Operations procedure to ensure that fuel is transferred before its use is required.

Operations procedure to ensure that fuel is transferred before its use is required.

Operations procedure to ensure System is not required.

Operations procedure to ensure System is not required.

Operations procedure to ensure System is not required.

Operations procedure to ensure Fuselage Cap is visually checked for security.

Maintenance procedure to secure or deactivate Pump.

Operations procedure to ensure its use is not required.

Operations procedure to establish alternate methods for recording flight time.

Maintenance procedure to secure or deactivate Anti-Skid System and determine Nose Wheel Steering operates normally.

Operations procedure to ensure Anti-Skid System is not required.

Operations procedure to ensure ground deicing procedures do not require their use.

Operations procedure to ensure passengers are briefed on use of Seat Belts and smoking privileges.

Maintenance procedure to research the appropriate listed documents to ensure an acceptable level of lighting is available.

Operations procedure to ensure approach procedures do not require its use.

Operations procedure to ensure altitude clearances are monitored.

DEPARTMENT OF TRANSPORTATION

  34-18

(O)

(O)

(O)

34-20

(O)

34-22

(M)

(M)

34-23

(M)

(M)

34-23-2

(O)

34-23-3

(O)

34-35

(O)

(O)

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXVIII

Guidelines for (O) & (M) Procedures

Operations procedure to ensure three Compass Systems are operative.

Operations procedure to ensure two independent Compass Systems are operative and aircraft is operated under positive radar control the entire flight.

Operations procedure to ensure aircraft is operated with a minimum of two independent Compass Systems in conjunction with approved Free Gyro Navigation Techniques.

Operations procedure to determine SAT/TAS data are either available or not required by other required Systems and applicable FAR does not require SAT/TAS System for the operation(s) conducted.

Maintenance procedure to deactivate and secure the System.

Maintenance procedure to deactivate and secure the System.

Maintenance procedure to deactivate and secure the System.

Maintenance procedure to deactivate and secure the System.

Operations procedure to ensure TA ONLY mode is selected and all TA functions/elements are operative and enroute and approach procedures do not require its use.

Operations procedure to ensure all RA display and audio functions are operative and enroute and approach procedures do not require its use.

Operations procedure to evaluate operations without Weather Radar available.

34-38-A-1

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-A-1-a

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

DEPARTMENT OF TRANSPORTATION

  (O)

(O)

(O)

(O)

(O)

(O)

(O)

(O)

(O)

(O)

(O)

34-39-1

(O)

34-39-2

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXIX

Guidelines for (O) & (M) Procedures

34-38-A-1-d

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-A-1-e

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

Operations procedures to establish to ensure crew awareness of aircraft altitude, performance and normal operation of the Windshear Detection  and Avoidance System (Predictive).

34-38-A-2

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-B-1

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-B-1-a

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-B-1-d

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance when Advisory Callouts are not required by FAR.

34-38-B-1-e

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

34-38-C-1

Operations procedures to establish to ensure crew awareness of aircraft altitude and performance.

Operations procedure to establish and use alternate procedures including reviewing windshear avoidance and windshear recovery procedures.

Operations procedure to establish and use alternate procedures including reviewing windshear avoidance and windshear recovery procedures.

DEPARTMENT OF TRANSPORTATION

  34-40-1

(O)

34-41-1

(O)

38-1

(M)

(M)

38-2

(M)

(M)

52-1

(O)

73-1

(O)

78-1-1

(M)

(O)

78-1-2

(M)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

REVISION: 6

DATE: 11/30/2006

PAGE NO:

XXX

Guidelines for (O) & (M) Procedures

Operations procedure to verify status and suitability of Navigation Facilities.

Operations procedure to verify status and suitability of Navigation Facilities.

Maintenance procedure to deactivate the associated components and verify there are no leaks in the Potable Water System.

Maintenance procedure to drain Potable Water System and ensure the System is not serviced prior to repair.

Maintenance procedure to deactivate or isolate the associated components and verify there are no leaks in the Lavatory Waste System.

Maintenance procedure to deactivate or isolate the associated components, verify there are no leaks in the Lavatory Waste System and the Door is placarded.

Operations procedure to ensure a crewmember visually verifies Door security.

Operations procedure to ensure Fuel Flow Indicating System is not required.

Maintenance procedure to secure the affected Thrust Reverser.

Operations procedure to evaluate operations with one Thrust Reverser stowed.

Maintenance procedure to secure both Thrust Reversers.

DEPARTMENT OF TRANSPORTATION

  21-1

1

0

1

0

a)

b)

1

0

1

0

1

0

a)

b)

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 6

DATE:  11/30/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

1. Cabin Pressurization

System

1) Automatic Dual Emergency Pressurization System Without Override Switches

C

May be inoperative provided aircraft is operated at or below 9,000 feet MSL.

C

(O) May be inoperative provided:

Aircraft is operated in an unpressurized configuration or Aircraft is operated at or below

|

|

|

9,000 feet MSL.

|

C

(O)May be inoperative provided procedures ensure that bleed air inflow to the cabin is operative and ON (Cabin Bleed and Cabin Air Switch(es) ON as appropriate to aircraft configuration).

2) Manually Actuated Emergency Pressurization System

C

May be inoperative provided aircraft is operated at or below 9,000 feet MSL.

C

(O) May be inoperative provided:

Aircraft is operated in an unpressurized configuration or Aircraft is operated at or below

|

|

|

9,000 feet MSL.

|

C

(O) May be inoperative provided procedures ensure that bleed air inflow to the Cabin is operative and ON (Cabin Bleed and Cabin Air Switch(es) ON as appropriate to aircraft configuration).

(continued)

DEPARTMENT OF TRANSPORTATION

  21-2

1

0

a)

b)

1

0

1

0

a)

b)

3.

1

0

a)

b)

4.

1

0

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 6

DATE: 11/30/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

1. Cabin Pressurization

System (Continued)

3) Automatic Dual Emergency Pressurization System With Override Switches

B

May be inoperative provided:

Aircraft is operated in an unpressurized configuration and Aircraft is operated at or below

|

|

|

9,000 feet MSL

|

B

(O) May be inoperative provided procedures are established to ensure that Override Switches are in OVERRIDE.

NOTE:  Passenger Oxygen Mask Auto Deployment will function at appropriate altitude unless PASS OXY Valve in the Cockpit remains OFF.

|

2. Cabin Pressurization Control System (Automatic Mode)

C

May be inoperative provided:

Autopilot is operative and Aircraft is operated at or below 25,000 feet MSL.

Cabin Air Outflow Valve 24, 25, 28, 29, 35, 36) Cabin Exhaust Control Valve (55)

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

Cabin Pressure Safety

Valve

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

DEPARTMENT OF TRANSPORTATION

  21-3

2

0

a)

b)

1)

2

1

a)

b)

c)

2)

2

1

a)

b)

c)

6.

2

0

a)

b)

2

1

2

0

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 5

DATE: 11/22/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

5. Cabin Differential

Pressure Relief Valves

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

(24, 25, 28, 29, 35, 36)

C

One may be inoperative provided:

Aircraft is operated at or below 25,000 feet MSL,

Cabin Air Outflow Valve is

operative and

Cabin Differential Pressure

Gauge is operative.

(55)

C

One may be inoperative provided:

Aircraft is operated at or below 25,000 feet MSL,

Cabin Exhaust Control Valve

is operative and

Cabin Differential Pressure

Gauge is operative.

Cabin Altitude Limiters

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

C

One may be inoperative provided aircraft is operated at or below 25,000 feet MSL.

7. Emergency

Pressurization Bleed Air Shutoff Valves (All Models With Dual Emergency Pressurization System)

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative, Aircraft is operated at or below 9,000 feet MSL and

Aircraft is not flown in known or forecast icing conditions.

(continued)

DEPARTMENT OF TRANSPORTATION

  21-4

21

2

1

a)

b)

1

0

9.

1

0

1

0

1

0

a)

b)

1

0

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 4

DATE: 04/04/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

AIR CONDITIONING

7. Emergency

Pressurization Bleed Air Shutoff Valves (All Models With dual Emergency Pressurization System) (Continued)

C

One may be inoperative provided:

Aircraft is operated at or below 25,000 feet MSL and

Aircraft is not flown in known or forecast icing conditions.

8. Emergency

Pressurization Light (All Models With Dual Emergency Pressurization System)

C

(M) May be inoperative provided maintenance procedures verify that both Emergency Pressurization Systems are operative before each flight.

Cabin Altitude Aural

Warning System

C

May be inoperative provided aircraft is operated at or below 10,000 feet MSL.

C

May be inoperative provided Cabin Pressurization System is considered inoperative.

10.  Cabin Altimeter

C

May be inoperative provided:

Cabin Differential Pressure

Gauge is operative and

A chart is provided to convert Cabin differential pressure to Cabin altitude.

C

(O) May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

DEPARTMENT OF TRANSPORTATION

  21-5

1

0

a)

b)

1

0

a)

b)

1

0

a)

b)

c)

1

0

1)

36)

1

0

2)

2

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 6

DATE: 11/30/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

11. Cabin Differential

Pressure Gauge

C

May be inoperative provided:

Cabin Altimeter is operative

and

A chart is provided to convert Cabin altitude to Cabin differential pressure.

C

(O) May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

12.  Cabin Rate of Climb Indicator

C

May be inoperative provided:

Cabin Altimeter is operative,

Cabin Differential Pressure

|

Gauge is operative and Cabin Pressurization Control System Automatic Mode is operative.

C

May be inoperative provided aircraft is operated at or below 9,000 feet MSL.

13. Automatic Temperature

Control Systems

Cabin (24, 25, 28, 29, 35,

C

May be inoperative provided Manual

Temperature Control System is operative.

Cockpit and Cabin (55)

C

May be inoperative provided Manual

Temperature Control System is operative.

DEPARTMENT OF TRANSPORTATION

  21-6

1)

36)

1

0

2)

2

0

1)

1

0

2)

55

2

0

1

0

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 5

DATE: 11/22/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

14. Manual Temperature

Control Systems

Cabin (24, 25, 28, 29, 35,

C

May be inoperative provided Automatic

Temperature Control System is operative.

Cockpit and Cabin (55)

C

May be inoperative provided Automatic

Temperature Control System is operative.

15. Temperature Control

Valve Indicator

(For H-Valve)

24, 25, 28, 29, 35, 36

C

May be inoperative provided Automatic Temperature Control Systems or Manual Temperature Control Systems for both Cockpit and Cabin are operative.

C

May be inoperative provided Automatic Temperature Control Systems or Manual Temperature Control Systems for both Cockpit and Cabin are operative.

16.  Cooling System

***

(Freon)

1) Cabin

C

2) Cockpit

C

17.  Cabin Temperature

***

Indicator

C 1 0

18.  Cabin Ventilation Fan

C

DEPARTMENT OF TRANSPORTATION

  21-7

1

0

36)

2

1

a)

b)

2

0

a)

b)

c)

1

0

1

0

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

LR-24, -25, -28, -29, -35, -36, -55

SYSTEM

REVISION NO: 5

DATE: 11/22/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

19.  Cockpit Ventilation Fan

C

20.  Auxiliary Cockpit and

***

Cabin Heaters

C - 0

21.  Engine Bleed Air

Modulating Valves (35,

Engine Bleed Air Mixing

Valves (55)

C

One may be inoperative provided:

Aircraft is operated at or below 25,000 feet MSL and

Aircraft is not operated in known or forecast icing conditions.

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative, Aircraft is not flown in known or forecast icing conditions and

Aircraft is operated at or below 9,000 feet MSL.

22.  Auxiliary Defog System

***

C

23. Cabin Pressurization

Control System (Manual

Mode)

C

May be inoperative provided:

Cabin Pressurization System is considered inoperative and Aircraft is operated at or below 9,000 feet MSL.

DEPARTMENT OF TRANSPORTATION

  22-1